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WO2018032416A1 - Procédé et système de commande de la vitesse de rotation d'un véhicule aérien sans pilote - Google Patents

Procédé et système de commande de la vitesse de rotation d'un véhicule aérien sans pilote Download PDF

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Publication number
WO2018032416A1
WO2018032416A1 PCT/CN2016/095709 CN2016095709W WO2018032416A1 WO 2018032416 A1 WO2018032416 A1 WO 2018032416A1 CN 2016095709 W CN2016095709 W CN 2016095709W WO 2018032416 A1 WO2018032416 A1 WO 2018032416A1
Authority
WO
WIPO (PCT)
Prior art keywords
remaining power
drone
speed range
speed
present
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/CN2016/095709
Other languages
English (en)
Chinese (zh)
Inventor
张琬彬
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to PCT/CN2016/095709 priority Critical patent/WO2018032416A1/fr
Publication of WO2018032416A1 publication Critical patent/WO2018032416A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/36—Arrangements for testing, measuring or monitoring the electrical condition of accumulators or electric batteries, e.g. capacity or state of charge [SoC]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls

Definitions

  • the invention relates to the field of drones, and in particular to a method and system for controlling the speed of a drone.
  • the drone is an unmanned aircraft. Because it does not require a cockpit, its size can be made small.
  • the existing drones are generally powered by batteries. The existing drones cannot use the battery to calculate the speed. Adjustment, resulting in a large loss of power, affecting the user's experience.
  • a method for controlling the speed of a drone is provided, which solves the disadvantage of low user experience in the prior art.
  • a method for controlling a rotational speed of a drone comprising the steps of:
  • the drone speed is controlled within the speed range corresponding to the remaining power.
  • the method further includes:
  • the method further includes:
  • the user is received feedback of the speed range, and the speed range is adjusted according to the feedback.
  • a speed control system for a drone comprising:
  • a detecting unit for detecting the remaining power of the drone
  • a determining unit configured to determine whether the remaining power is lower than a set threshold
  • the control unit is configured to control the speed of the drone within the speed range corresponding to the remaining power.
  • system further includes:
  • a sending unit for transmitting the speed range to the user.
  • system further includes:
  • the adjusting unit is configured to receive feedback from the user on the speed range, and adjust the speed range according to the feedback.
  • the technical solution provided by the specific embodiment of the present invention detects the remaining power of the drone.
  • the drone speed is controlled within the range of the corresponding power, so it has the advantage of improving the user experience. .
  • FIG. 1 is a flow chart of a method for controlling a rotational speed of a drone according to the present invention
  • FIG. 2 is a structural diagram of a rotational speed control system of a drone according to the present invention.
  • FIG. 1 is a flowchart of a method for controlling a rotational speed of a drone according to a first preferred embodiment of the present invention.
  • the method is implemented by a robot.
  • the method is as shown in FIG. 1 and includes the following steps:
  • Step S101 detecting remaining power of the drone
  • Step S102 determining whether the remaining power is lower than a set threshold
  • Step S103 When the remaining power is lower than the set threshold, control the drone rotation speed within the speed range corresponding to the remaining power.
  • the technical solution provided by the specific embodiment of the present invention detects the remaining power of the drone.
  • the drone speed is controlled within the range of the corresponding power, so it has the advantage of improving the user experience. .
  • the foregoing method may further include:
  • the foregoing method may further include:
  • the user is received feedback of the speed range, and the speed range is adjusted according to the feedback.
  • FIG. 2 is a rotation speed control system of a drone according to a second preferred embodiment of the present invention.
  • the system includes:
  • the detecting unit 201 is configured to detect a remaining power of the drone
  • the determining unit 202 is configured to determine whether the remaining power is lower than a set threshold
  • the control unit 203 is configured to control the speed of the drone within the speed range corresponding to the remaining power.
  • the technical solution provided by the specific embodiment of the present invention detects the remaining power of the drone.
  • the drone speed is controlled within the range of the corresponding power, so it has the advantage of improving the user experience. .
  • the above system may further include:
  • the sending unit 204 is configured to send the speed range to the user.
  • the above system may further include:
  • the adjusting unit 205 is configured to receive feedback from the user on the speed range, and adjust the speed range according to the feedback.
  • Computer readable media includes both computer storage media and communication media including any medium that facilitates transfer of a computer program from one location to another.
  • a storage medium may be any available media that can be accessed by a computer.
  • the computer readable medium may include random access memory (Random) Access Memory, RAM), Read-Only Memory (ROM), Electrically Erasable Programmable Read Only Memory (Electrically Erasable Programmable Read-Only Memory, EEPROM), Compact Disc Read-Only Memory, CD-ROM, or other optical disc storage, magnetic storage medium or other magnetic storage device, or any other medium that can be used to carry or store desired program code in the form of instructions or data structures and that can be accessed by a computer. Also. Any connection may suitably be a computer readable medium.
  • a disk and a disc include a compact disc (CD), a laser disc, a compact disc, a digital versatile disc (DVD), a floppy disk, and a Blu-ray disc, wherein the disc is usually magnetically copied, and the disc is The laser is used to optically replicate the data. Combinations of the above should also be included within the scope of the computer readable media.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

La présente invention concerne un procédé et un système de commande d'une vitesse de rotation de véhicule aérien sans pilote, le procédé comprenant les étapes suivantes consistant à: détecter le niveau de puissance restant d'un véhicule aérien sans pilote (S101); déterminer si le niveau de puissance restant est inférieur à une valeur de seuil prédéfinie (S102); lorsque le niveau de puissance restant est inférieur à la valeur de seuil prédéfinie, commander une vitesse de rotation du véhicule aérien sans pilote pour qu'elle se situe dans une plage de vitesse de rotation correspondant au niveau de puissance restant (S103). La présente invention présente l'avantage d'une expérience utilisateur élevée.
PCT/CN2016/095709 2016-08-17 2016-08-17 Procédé et système de commande de la vitesse de rotation d'un véhicule aérien sans pilote Ceased WO2018032416A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/CN2016/095709 WO2018032416A1 (fr) 2016-08-17 2016-08-17 Procédé et système de commande de la vitesse de rotation d'un véhicule aérien sans pilote

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2016/095709 WO2018032416A1 (fr) 2016-08-17 2016-08-17 Procédé et système de commande de la vitesse de rotation d'un véhicule aérien sans pilote

Publications (1)

Publication Number Publication Date
WO2018032416A1 true WO2018032416A1 (fr) 2018-02-22

Family

ID=61196434

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2016/095709 Ceased WO2018032416A1 (fr) 2016-08-17 2016-08-17 Procédé et système de commande de la vitesse de rotation d'un véhicule aérien sans pilote

Country Status (1)

Country Link
WO (1) WO2018032416A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109001647A (zh) * 2018-10-08 2018-12-14 成都戎创航空科技有限公司 一种无人机电池电量预警系统
CN112673330A (zh) * 2020-03-30 2021-04-16 深圳市大疆创新科技有限公司 无人机下降的控制方法和装置、无人机
CN120560326A (zh) * 2025-08-01 2025-08-29 国网浙江省电力有限公司 用于无人机追踪的飞行控制方法及系统

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104166355A (zh) * 2014-07-16 2014-11-26 深圳市大疆创新科技有限公司 电动无人机及其智能电量保护方法
CN105093130A (zh) * 2015-09-17 2015-11-25 杨珊珊 一种无人飞行器续航能力监测系统及方法
US20150336671A1 (en) * 2014-05-20 2015-11-26 Infatics, Inc. (DBA DroneDeploy) Method for adaptive mission execution on an unmanned aerial vehicle
CN105259917A (zh) * 2015-11-08 2016-01-20 杨珊珊 一种无人飞行器安全快速降落装置及方法
CN105398578A (zh) * 2015-11-12 2016-03-16 中国人民解放军国防科学技术大学 一种基于纵向航迹的太阳能飞行器安全控制方法
CN106275463A (zh) * 2016-08-17 2017-01-04 张琬彬 无人机的转速控制方法及系统

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150336671A1 (en) * 2014-05-20 2015-11-26 Infatics, Inc. (DBA DroneDeploy) Method for adaptive mission execution on an unmanned aerial vehicle
CN104166355A (zh) * 2014-07-16 2014-11-26 深圳市大疆创新科技有限公司 电动无人机及其智能电量保护方法
CN105093130A (zh) * 2015-09-17 2015-11-25 杨珊珊 一种无人飞行器续航能力监测系统及方法
CN105259917A (zh) * 2015-11-08 2016-01-20 杨珊珊 一种无人飞行器安全快速降落装置及方法
CN105398578A (zh) * 2015-11-12 2016-03-16 中国人民解放军国防科学技术大学 一种基于纵向航迹的太阳能飞行器安全控制方法
CN106275463A (zh) * 2016-08-17 2017-01-04 张琬彬 无人机的转速控制方法及系统

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109001647A (zh) * 2018-10-08 2018-12-14 成都戎创航空科技有限公司 一种无人机电池电量预警系统
CN112673330A (zh) * 2020-03-30 2021-04-16 深圳市大疆创新科技有限公司 无人机下降的控制方法和装置、无人机
CN112673330B (zh) * 2020-03-30 2024-05-14 深圳市大疆创新科技有限公司 无人机下降的控制方法和装置、无人机
CN120560326A (zh) * 2025-08-01 2025-08-29 国网浙江省电力有限公司 用于无人机追踪的飞行控制方法及系统

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